CN205342475U - Aircraft finish machining platform - Google Patents

Aircraft finish machining platform Download PDF

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Publication number
CN205342475U
CN205342475U CN201620159173.2U CN201620159173U CN205342475U CN 205342475 U CN205342475 U CN 205342475U CN 201620159173 U CN201620159173 U CN 201620159173U CN 205342475 U CN205342475 U CN 205342475U
Authority
CN
China
Prior art keywords
wing
fuselage
processing stations
polish
machining
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn - After Issue
Application number
CN201620159173.2U
Other languages
Chinese (zh)
Inventor
田俊
梁星鑫
王浩亮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ZHEJIANG RIFA AVIATION DIGITAL EQUIPMENT Co Ltd
Original Assignee
ZHEJIANG RIFA AVIATION DIGITAL EQUIPMENT Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by ZHEJIANG RIFA AVIATION DIGITAL EQUIPMENT Co Ltd filed Critical ZHEJIANG RIFA AVIATION DIGITAL EQUIPMENT Co Ltd
Priority to CN201620159173.2U priority Critical patent/CN205342475U/en
Application granted granted Critical
Publication of CN205342475U publication Critical patent/CN205342475U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides an aircraft finish machining platform, belongs to the smart processing technology field of aircraft. The utility model discloses a set up in the fuselage machining -position progressive and the wing machining -position progressive of finish machining bench, respectively to being applied to finish machining aircraft fuselage and wing, fuselage machining -position progressive is provided with fuselage strutting arrangement, the appearance unit is transferred to the fuselage, fuselage positioner, fuselage finish machining host computer, fuselage finish machining special plane and fuselage machining -position progressive master control junction center, be provided with the wing support bracket among the wing machining -position progressive, the appearance unit is transferred to the wing, wing positioner, wing finish machining host computer and wing machining -position progressive master control junction center, fuselage machining -position progressive master control junction center and wing machining -position progressive master control junction center set up in wing machining -position progressive's right side, fuselage machining -position progressive master control junction center and wing machining -position progressive master control junction center form the control relation of host computer to the next machine.

Description

A kind of aircraft finishing station
Technical field
This utility model belongs to aircraft finishing technology field, especially relevant with a kind of aircraft finishing station.
Background technology
Existing China's Aviation Industry was through the development of more than 50 years, have been provided with producing technology and the material base of various aircraft, aircraft polish is again an extremely important ring in aircraft manufacturing link, especially the various crossing point holes on airframe and wing, nipple orifice, dead eye, machining accuracy and the efficiency requirements of connecting end surface etc. are higher, accurately machined precision and efficiency determine the final mass of aircraft to a great extent, manufacturing cost and cycle, existing domestic aircraft polish is usually branch and is processed, need to carry out multiple clamping location, such as airframe, the separate machined such as wing, add man-hour in Set and Positioning process, have certain error, assembly precision is affected after multiple error is accumulative, affect Aircraft Quality, simultaneously inefficient.
Utility model content
The purpose of this utility model is intended to overcome existing defect, it is provided that a kind of machining accuracy is high, the aircraft finishing station of excellent in efficiency.
For this, this utility model is by the following technical solutions: a kind of aircraft finishing station, it is characterized in that, described finishing station includes the fuselage processing stations and the wing processing stations that are arranged in finishing station, respectively to being applied to polish airframe and wing, described fuselage processing stations is provided with body supporting apparatus, fuselage attitude-adjusting unit, fuselage positioner, fuselage polish main frame, fuselage polish special plane and fuselage processing stations Master Control Center station, body supporting apparatus includes forebody bracket and rear body bracket, described forebody bracket and rear body bracket are supported by a described fuselage attitude-adjusting unit respectively and install, each fuselage attitude-adjusting unit forms by 4 digital control location devices, 4 digital control location devices are arranged together in two row and arrange along course, described fuselage positioner includes the laser tracker being divided into described fuselage processing stations both sides, described polish main frame is used for processing crossing point holes and connecting end surface, polish special plane is for processing the processing of dead eye and connecting end surface, fuselage processing stations Master Control Center station is arranged at the right side of described fuselage processing stations;Described wing processing stations is provided with wing Support bracket, wing attitude-adjusting unit, wing positioner, wing polish main frame and wing processing stations Master Control Center station, wing Support bracket is supported by described wing attitude-adjusting unit and installs, wing attitude-adjusting unit is made up of along course distribution three digital control location devices, described wing positioner includes the laser tracker being divided into described wing processing stations both sides, wing polish main frame is used for working joint hole and connecting end surface, described wing processing stations Master Control Center station is arranged at the right side of described wing processing stations, described fuselage processing stations Master Control Center station and wing processing stations Master Control Center station form the host computer control planning to slave computer, realize the management that work flow is integrated and ordered.
As supplementing and perfect technique scheme, this utility model also includes techniques below feature.
Described wing attitude-adjusting unit is provided with two the corresponding port wing supporting clamping aircraft and starboard wings respectively along course distribution.
Described fuselage polish main frame, polish special plane and wing polish main frame can realize five-axle linkage, and then meet the processing request of relevant hole dough-making powder.
This utility model can reach following beneficial effect: by the layout being used for processing the digitized finishing station of aircraft is divided into fuselage processing stations and two stations of wing processing stations, airframe and wing are integrated in same finishing station and realize aircraft digital polish, improve work efficiency and machining accuracy;And digitized Finish Machining System of the present utility model can meet multi-model rapid interchangeable, it is only necessary to according to different type of machines, change corresponding bracket;Before and after fuselage adopt localizer to be equally spaced, it is possible to before and after meeting, the station of fuselage exchanges, and carries out keeping in repair or during regular inspection at a machine tool, it is ensured that the seriality of production;The accurately mobile of three directions and location can be realized by 4 (or 3) localizers, it is achieved fuselage, wing pose adjustment;Fuselage processing stations and wing processing stations adopt multiple stage laser tracker, it is achieved to being accurately positioned of fuselage and wing.
Accompanying drawing explanation
Fig. 1 is main apparent direction schematic diagram of the present utility model.
Fig. 2 is side-looking direction of the present utility model schematic diagram.
Detailed description of the invention
Below in conjunction with accompanying drawing, detailed description of the invention of the present utility model is described in detail.
As depicted in figs. 1 and 2, this utility model includes the fuselage processing stations and the wing processing stations that are arranged in finishing station 1, respectively to being applied to polish airframe and wing 11, described fuselage processing stations is provided with body supporting apparatus, fuselage attitude-adjusting unit, fuselage positioner, fuselage polish main frame 9, fuselage polish special plane 4 and fuselage processing stations Master Control Center station 5, body supporting apparatus includes forebody bracket 7 and rear body bracket, the forebody 10 of the corresponding clamping aircraft of difference and rear body 8, described forebody bracket 7 and rear body bracket 13 are supported by a described fuselage attitude-adjusting unit respectively and install, each fuselage attitude-adjusting unit forms by 4 digital control location devices 6, 4 digital control location devices 6 are arranged together in two row and are arranged in finishing station 1 along course, described forebody bracket 7 and rear body bracket 13 are connected with digital control location device 6 each through process connection, indirectly realize support and the pose adjustment of assembling object, each digital control location device 6 can realize the accurately mobile of three directions and location, realize fuselage, the pose adjustment of wing, described fuselage positioner includes the laser tracker 16 being divided into described fuselage processing stations both sides, polish main frame 9 is used for processing crossing point holes and connecting end surface, polish special plane 4 is for processing the processing of dead eye and connecting end surface, fuselage processing stations Master Control Center station 5 is arranged at the right side of described fuselage processing stations;Described wing processing stations arranges wing attitude-adjusting unit, wing positioner, wing polish main frame 12 and wing processing stations Master Control Center station 2, wing attitude-adjusting unit is provided with two along course distribution, correspondence supports port wing 14 and the starboard wing 11 of clamping aircraft respectively, each wing attitude-adjusting unit is made up of along course distribution three digital control location devices 3, described wing positioner includes the laser tracker 15 being divided into described wing processing stations both sides, wing polish main frame 12 is for working joint hole and connecting end surface, described wing processing stations Master Control Center station 2 is arranged at the right side of described wing processing stations, described fuselage processing stations Master Control Center station 5 and wing processing stations Master Control Center station 2 form the host computer control planning to slave computer, namely when left and right wing is when polish, Working position and the process data at wing processing stations Master Control Center station 2 is controlled by fuselage processing stations Master Control Center station 5, realize the management that work flow is integrated and ordered.
The step that this utility model is implemented is: 1. forebody bracket 7 enters position;2. rear body bracket 13 enters position;3. forebody 10 is added;4. rear body 8 is added;5. forebody processing stations is measured;6. rear body processing stations is measured;7. forward and backward fuselage posture adjustment;8. forward and backward fuselage locking, fixing;9. forward and backward fuselage polish;10. undercarriage dead eye and connecting end surface processing;11. port wing 14 and starboard wing 11 enter position;12. wing processing stations is measured;13. left and right wing posture adjustment;14. the locking of left and right wing, fixing;15. left and right wing polish;16. forward and backward fuselage undercarriage;16. left and right wing undercarriage.

Claims (3)

1. an aircraft finishing station, it is characterized in that: described finishing station includes the fuselage processing stations and the wing processing stations that are arranged in this finishing station, respectively to being applied to polish airframe and wing, described fuselage processing stations is provided with body supporting apparatus, fuselage attitude-adjusting unit, fuselage positioner, fuselage polish main frame, fuselage polish special plane and fuselage processing stations Master Control Center station, body supporting apparatus includes forebody bracket and rear body bracket, described forebody bracket and rear body bracket are supported by a described fuselage attitude-adjusting unit respectively and install, each fuselage attitude-adjusting unit forms by 4 digital control location devices, 4 digital control location devices are arranged together in two row and arrange along course, described fuselage positioner includes the laser tracker being divided into described fuselage processing stations both sides, described polish main frame is used for processing crossing point holes and connecting end surface, polish special plane is for processing the processing of dead eye and connecting end surface, fuselage processing stations Master Control Center station is arranged at the right side of described fuselage processing stations;Described wing processing stations is provided with wing Support bracket, wing attitude-adjusting unit, wing positioner, wing polish main frame and wing processing stations Master Control Center station, wing attitude-adjusting unit is made up of along course distribution three digital control location devices, described wing positioner includes the laser tracker being divided into described wing processing stations both sides, wing polish main frame is used for working joint hole and connecting end surface, described wing processing stations Master Control Center station is arranged at the right side of described wing processing stations, described fuselage processing stations Master Control Center station and wing processing stations Master Control Center station form the host computer control planning to slave computer.
2. a kind of aircraft finishing station according to claim 1, it is characterised in that: described wing attitude-adjusting unit is provided with two the corresponding port wing supporting clamping aircraft and starboard wings respectively along course distribution.
3. a kind of aircraft finishing station according to claim 1, it is characterised in that: described fuselage polish main frame, polish special plane and wing polish main frame can realize five-axle linkage.
CN201620159173.2U 2016-03-02 2016-03-02 Aircraft finish machining platform Withdrawn - After Issue CN205342475U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620159173.2U CN205342475U (en) 2016-03-02 2016-03-02 Aircraft finish machining platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620159173.2U CN205342475U (en) 2016-03-02 2016-03-02 Aircraft finish machining platform

Publications (1)

Publication Number Publication Date
CN205342475U true CN205342475U (en) 2016-06-29

Family

ID=56181588

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620159173.2U Withdrawn - After Issue CN205342475U (en) 2016-03-02 2016-03-02 Aircraft finish machining platform

Country Status (1)

Country Link
CN (1) CN205342475U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105750933A (en) * 2016-03-02 2016-07-13 浙江日发航空数字装备有限责任公司 Digital fine machining table of airplane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105750933A (en) * 2016-03-02 2016-07-13 浙江日发航空数字装备有限责任公司 Digital fine machining table of airplane
CN105750933B (en) * 2016-03-02 2018-08-03 浙江日发航空数字装备有限责任公司 A kind of aircraft digital finishing station

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
AV01 Patent right actively abandoned
AV01 Patent right actively abandoned

Granted publication date: 20160629

Effective date of abandoning: 20180803